Vortex shedding past square cylinder
Vortex shedding past square cylinder URANS (K-Omega SST with no wall functions) – LES (Smagorinsky) – Vortices visualized by Q-criterion Vortices visualized by Q-criterion www.wolfdynamics.com/wiki/squarecil/les.gif www.wolfdynamics.com/wiki/squarecil/urans2.gif Laminar (no turbulence model) – Vortices DES (SpalartAllmarasDDES) – Vortices visualized by visualized by Q-criterion Q-criterion www.wolfdynamics.com/wiki/squarecil/laminar.gif www.wolfdynamics.com/wiki/squarecil/des.gif
Vortex shedding past square cylinder Turbulence model Drag coefficient Strouhal number Computing time (s) Laminar 2.81 0.179 93489 LES 2.32 0.124 77465 DES 2.08 0.124 70754 SAS 2.40 0.164 57690 URANS (WF) 2.31 0.130 67830 URANS (No WF) 2.28 0.135 64492 RANS 2.20 - 28246 (10000 iter) Experimental values 2.05-2.25 0.132 - Note: all simulations were run using 4 cores . References: D. A. Lyn and W. Rodi. “The flapping shear layer formed by flow separation from the forward corner of a square cylinder”. J. Fluid Mech., 267, 353, 1994. D. A. Lyn, S. Einav, W. Rodi and J. H. Park. “A laser -Doppler velocimetry study of ensemble-averaged characteristics of the turbulent near wake of a square cylinder”. Report. SFB 210 /E/100.
DLR-F6 aircraft model – RANS simulation
DLR-F6 aircraft model – RANS simulation
DLR-F6 aircraft model – RANS simulation
DLR-F6 aircraft model – RANS simulation
DLR-F6 aircraft model – RANS simulation
DLR-F6 aircraft model – RANS simulation
DLR-F6 aircraft model – RANS simulation
DLR-F6 aircraft model – RANS simulation
DLR-F6 aircraft model – RANS simulation
DLR-F6 aircraft model – RANS simulation
F1 in platoon formation – RANS simulation
F1 in platoon formation – RANS simulation
F1 in platoon formation – RANS simulation
F1 in platoon formation – RANS simulation
F1 in platoon formation – RANS simulation
F1 in platoon formation – RANS simulation
Recommend
More recommend